View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 61718U 26145.54510356 +.00000000 +00000-0 +16114-5 0 00001
2 61718 53.1608 90.8146 0001175 89.6882 270.4256 15.34386190 07
| Epoch (UTC): | 25 May 2026 13:04:56 |
| Eccentricity: | 0.0001175 |
| inclination: | 53.1608° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 90.8146° |
| argument of perigee: | 89.6882° |
| revolutions per day: | 15.34386190 |
| mean anomaly at epoch: | 270.4256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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